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西北工业大学 国内
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Autonomous Cooling Design and Temperature Control Mechanism of Hypersonic Vehicle
Lin Wang, Rui Ma,
Bing Liu
, Shibin Li
National University of Defense Technology
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Engineering
Control System
100%
Cooling Device
100%
Flow Direction
50%
Hypersonic Vehicle
50%
Liquid Phase
50%
Mixing Zone
50%
Numerical Method
50%
Thermal Control
50%
Transients
50%
Two-Phase Flow
50%
Physics
Hypersonic Vehicle
50%
Liquid Phase
50%
Mathematical Method
50%
Temperature Control
100%
Transients
50%
Two Phase Flow
50%
Vapor Phase
100%
Working Fluid
50%
Material Science
Pore Structure
100%
Two Phase Flow
100%